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Volume 19, Issue 2
1 February 1947
This article was originally published in
Aircraft Engineering
Aircraft Engineering Cover Image for Volume 19, Issue 2
Review Article| February 01 1947

The Stresses in Cylindrical Vessels

H.D. Conway, M.A., Ph.D.
H.D. Conway, M.A., Ph.D.
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Author & Article Information
Publisher: Emerald Publishing
Online ISSN: 2059-9366
Print ISSN: 0002-2667
© MCB UP Limited
1947
Aircraft Engineering (1947) 19 (2): 52–54.
https://doi.org/10.1108/eb031472

USING the general theory of cylindrical shells, expressions have been derived for the maximum bending moment and shearing force in vessels closed at one end and subjected internally to (a) gas pressure, (b) hydrostatic pressure. The method has been used by S. Timoshenko (Theory of Plates and Shells, McGraw‐Hill, pp. 412–3) for the special case where one end of the vessels is built into a rigid foundation.

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© MCB UP Limited
1947
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